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火箭技术

铝颗粒在多相流中燃烧的数值模拟

  • 刘丛林 ,
  • 郜冶 ,
  • 贺征
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  • 哈尔滨工程大学航天与建筑工程学院,哈尔滨 150001

刘丛林(1981-),女,吉林人,博士研究生,研究方向:固体火箭发动机燃烧与流动。

收稿日期: 2011-10-08

  网络出版日期: 2025-05-29

基金资助

中央高校基本科研业务费专项资金(HEUCF100201)

The Numerical Simulation of Aluminum Droplet Combustion in Multi-phase Fluid

  • LIU Conglin ,
  • GAO Ye ,
  • HE Zheng
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  • College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, china

Received date: 2011-10-08

  Online published: 2025-05-29

摘要

铝颗粒的燃烧细节决定着推进剂的性能。应用Fick第一定律及Fourier定律,对燃烧颗粒中各组分气体的质量与能量扩散过程进行计算,跟踪氧化反应中生成的中间态产物,总结了颗粒尺寸及组分随燃烧时间的变化规律,以及颗粒的燃烧效率等。结果表明,颗粒燃烧初期,反应进行的较为强烈,约60ms后,燃烧趋于平稳,最终,颗粒20%以上的外表面被氧化物所覆盖。

本文引用格式

刘丛林 , 郜冶 , 贺征 . 铝颗粒在多相流中燃烧的数值模拟[J]. 弹箭与制导学报, 2012 , 32(3) : 118 -120,124 . DOI: 10.15892/j.cnki.djzdxb.2012.03.029

Abstract

The aluminum droplet's burning detail is important for propellant capability. Based on Fick's first law and Fourier law, the mass and energy diffusion process between gases produced by burning aluminum droplet was computed. Following the track of the intermediate product, the development of droplet's size, component, and combustion efficiency were studied. Results show that in early process, the reaction is more intense. After 60 ms, the burning becomes placid. Finally, about 20% of the droplet surface is covered by the oxide cap.

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